| タイトル | Pressure-Equalizing Cradle for Booster Rocket Mounting |
| 本文（外部サイト） | http://hdl.handle.net/2060/20150003464 |
| 著者（英） | Rutan, Elbert L. |
| 発行日 | 2015-02-24 |
| 言語 | eng |
| 内容記述 | A launch system and method improve the launch efficiency of a booster rocket and payload. A launch aircraft atop which the booster rocket is mounted in a cradle, is flown or towed to an elevation at which the booster rocket is released. The cradle provides for reduced structural requirements for the booster rocket by including a compressible layer, that may be provided by a plurality of gas or liquid-filled flexible chambers. The compressible layer contacts the booster rocket along most of the length of the booster rocket to distribute applied pressure, nearly eliminating bending loads. Distributing the pressure eliminates point loading conditions and bending moments that would otherwise be generated in the booster rocket structure during carrying. The chambers may be balloons distributed in rows and columns within the cradle or cylindrical chambers extending along a length of the cradle. The cradle may include a manifold communicating gas between chambers. |
| NASA分類 | Launch Vehicles and Launch Operations |
| 権利 | No Copyright |
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